17,005 Documents in our Technical Library
2458383 Total Downloads

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

AA-SM-026-008

  • Version
  • 1027 Downloads
  • 109.80 KB File Size
  • 2 File Count
  • September 18, 2016 Create Date
  • January 16, 2022 Last Updated
Scroll for Details

AA-SM-026-008 Beam Analysis - Cantilever - Triangular load Part Span Peak at Free End

Free Engineering Spreadsheets: Beam analysis spreadsheet, based on the method in NASA-TM-73305, the NASA Stress Analysis Manual. Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

aa-sm-026-008


16 January 2022 - Rev A added, corrected calculation for theta

FileAction
AA-SM-026-008 Beam Analysis - Cantilever - Triangle load Part Span Peak at Free End - Rev A.xlsxDownload 
AA-SM-026-008 Beam Analysis - Cantilever - Triangle load Part Span Peak at Free End.xlsxDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

AA-SM-026-008

  • Version
  • 1027 Downloads
  • 109.80 KB File Size
  • 2 File Count
  • September 18, 2016 Create Date
  • January 16, 2022 Last Updated
Scroll for Details

AA-SM-026-008 Beam Analysis - Cantilever - Triangular load Part Span Peak at Free End

Free Engineering Spreadsheets: Beam analysis spreadsheet, based on the method in NASA-TM-73305, the NASA Stress Analysis Manual. Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

aa-sm-026-008


16 January 2022 - Rev A added, corrected calculation for theta

FileAction
AA-SM-026-008 Beam Analysis - Cantilever - Triangle load Part Span Peak at Free End - Rev A.xlsxDownload 
AA-SM-026-008 Beam Analysis - Cantilever - Triangle load Part Span Peak at Free End.xlsxDownload 
17,005 Documents in our Technical Library
2458383 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...